unit 1 Flashcards

1
Q

What is the composition of JP-8 fuel?

A

Gasoline and kerosene

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2
Q

At room temperature, how many times longer will it take water to settle out of JP-8 than out of gasoline?

A

Four

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3
Q

Jet aircraft operating at moderately high altitudes increase the fuel system’s susceptibility to an icing condition, further aggravated by the

A

higher viscosity of jet fuels

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4
Q

The main fuel control allows the jet engine to safely accelerate, reducing the possibility of

A

flameout

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5
Q

During a visual inspection, how can you tell when a fuel filter is clogged?

A

A differential pressure indicator is actuated

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6
Q

On a dual-spool, axial-flow engine, what controls thrust production of the engine?

A

Controlling turbine inlet temperature

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7
Q

During jet engine deceleration, a hydro mechanical fuel control schedules fuel flow as a function of

A

burner pressure

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8
Q

what type of fuel control uses items such as thermocouples, relays, amplifiers, and solenoids to help control a jet engine?

A

Electrohydromechanical

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9
Q

Which term describes a jet engine fuel metering device that is really two fuel controls in one component?

A

Unified

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10
Q

The F100 UFC senses certain variables from the engine through the use of

A

a closed loop design

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11
Q

If the safety seals on a fuel system component are broken or removed, and you suspect the factory adjustment was altered, you should

A

forward the component to the authorized depot fro reflow and resealing

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12
Q

Calibration and/or adjustment screws that require setting during an engine trim procedure must be

A

safety sealed and/or lockwired

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13
Q

When in the primary mode, what controls the operation of the F100-PW-200 engine?

A

DEEC

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14
Q

On an F100-PW-220 engine, the DEEC is cooled by

A

fuel

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15
Q

For actuation of the variable van systems on an F100-PW-220 engine, the MFC provides both the CIVV and

A

rear compressor variable van actuators with fuel pressure

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16
Q

Which F100-PW-220 engine fuel system component controls pressurization of the core engine fuel system?

A

P&D valve

17
Q

Which stage of compressor air drives the augmenter fuel pump on an F100-PW-220 engine?

A

13th

18
Q

On the F100-PW-220 engine which component controls the augmentor fuel control

A

DEEC

19
Q

Core engine fuel flow sequence on an F100-P@-220 engine starts at the main fuel pump and then goes through the

A

MFC, fuel/oil cooler, P&D, and fuel nozzles